Skip to content
Merged
Show file tree
Hide file tree
Changes from all commits
Commits
File filter

Filter by extension

Filter by extension

Conversations
Failed to load comments.
Loading
Jump to
Jump to file
Failed to load files.
Loading
Diff view
Diff view
24 changes: 16 additions & 8 deletions README.md
Original file line number Diff line number Diff line change
Expand Up @@ -25,8 +25,8 @@ It will often be combined with other extensions that describe the actual data, s
| ------------------------------------- | --------------------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
| sat:platform_international_designator | string | The International Designator, also known as COSPAR ID, and NSSDCA ID |
| sat:orbit_state | string | The state of the orbit. Either `ascending` or `descending` for polar orbiting satellites, or `geostationary` for geosynchronous satellites |
| sat:absolute_orbit | integer | The absolute orbit number at the time of acquisition. |
| sat:relative_orbit | integer | The relative orbit number at the time of acquisition. |
| sat:absolute_orbit | integer | The absolute orbit number at the start of acquisition. |
| sat:relative_orbit | integer | The relative orbit number at the start of acquisition. |
| sat:orbit_cycle | integer | The number of repeat cycle done by the satellite at the time of the acquisition. [Repeat cycle](https://ltb.itc.utwente.nl/page/498/concept/81577) is the time between two successive identical orbits. |
| sat:orbit_state_vectors | Map<string, \[number]> | The state vectors of the satellite at the time of acquisition. |
| sat:anx_datetime | string | The [Ascending Node](https://en.wikipedia.org/wiki/Orbital_node) Crossing (ANX) time, in UTC. It is formatted according to [RFC 3339, section 5.6](https://tools.ietf.org/html/rfc3339#section-5.6). |
Expand All @@ -48,18 +48,26 @@ Indicates the type and current state of orbit. Satellites are either geosynchron

#### sat:absolute_orbit

A count of orbits from 1 to the number of orbits made in the total satellite lifecycle. In mission planning and tasking, the
absolute orbit may be used as a reference in the non systematic acquisition missions. The resulting Item can be tagged with the
absolute orbit and thus searchable as such. In the case of orbital changes during the mission modifying the ground track and
thus the repeat cycle and thus the number or relative orbits, the combination of cycle and relative orbit is not sufficient to
A count of orbits from 1 to the number of orbits made in the total satellite lifecycle. In mission planning and tasking, the
absolute orbit may be used as a reference in the non systematic acquisition missions. The resulting Item can be tagged with the
absolute orbit and thus searchable as such. In the case of orbital changes during the mission modifying the ground track and
thus the repeat cycle and thus the number or relative orbits, the combination of cycle and relative orbit is not sufficient to
derive an absolute orbit.

When the orbit changes during data acquisition (i.e., the acquisition spans multiple orbits), the convention is to use the
absolute orbit number at the start of the acquisition. This situation can occur, for example, in consolidated altimetry
products such as Sentinel-3.

#### sat:relative_orbit

A count of orbits from 1 to the number of orbits contained in a repeat cycle, where relative orbit 1 starts from a specific
reference location of the sub-satellite point (the point on the earth directly below the satellite). It resets to 1 when the
A count of orbits from 1 to the number of orbits contained in a repeat cycle, where relative orbit 1 starts from a specific
reference location of the sub-satellite point (the point on the earth directly below the satellite). It resets to 1 when the
sub-satellite point revisits the reference location.

When the orbit changes during data acquisition (i.e., the acquisition spans multiple orbits), the convention is to use the
relative orbit number at the start of the acquisition. This situation can occur, for example, in consolidated altimetry
products such as Sentinel-3.

#### sat:anx_datetime

The UTC time when the satellite crosses the [Ascending Node](https://en.wikipedia.org/wiki/Orbital_node). For geocentric and
Expand Down
4 changes: 4 additions & 0 deletions json-schema/schema.json
Original file line number Diff line number Diff line change
Expand Up @@ -124,10 +124,14 @@
]
},
"sat:absolute_orbit": {
"title": "Absolute Orbit",
"description": "The absolute orbit number at the start of acquisition. When the orbit changes during data acquisition (i.e., the acquisition spans multiple orbits), use the absolute orbit number at the start of the acquisition.",
"type": "integer",
"minimum": 1
},
"sat:relative_orbit": {
"title": "Relative Orbit",
"description": "The relative orbit number at the start of acquisition. When the orbit changes during data acquisition (i.e., the acquisition spans multiple orbits), use the relative orbit number at the start of the acquisition.",
"type": "integer",
"minimum": 1
},
Expand Down